A general procedure for obtaining velocity vector from a system of high response impact pressure probes
By: D. Adler and R. P. Shreeve
Contributors: Shreeve, Raymond P.; Naval Postgraduate School (U.S.)
Publisher: Naval Postgraduate School
Published: 1979
Place of publication: Monterey, California
Language: eng
Number of pages: 78
Subjects: Mathematical models; Turbomachines; Fluid dynamics; Pressure; Measurement
Description: A technique to measure a high frequency, repetitively pulsating flow field is presented. Two impact tube probes and a Kiel probe, all with pressure transducers mounted in thier tips are used. Five readings are required to identify a velocity vector at a point. In this report the technique, the numerical procedure and the computer program used are described.
Notes: "NPS-67-79-007"--Cover.

"July 1979"--Cover.

Title from cover.

"Prepared for: Naval Air Systems Command, Washington, DC and Office of Naval Research, Arlington, VA."

Includes bibliographical references (p. 54).

"Approved for public release; distribution is unlimited"--Cover.

Technical report; 1979.

ck/ 6/2/09.